First- and Second-Order Theory of Supersonic Flow Past Bodies of Revolution
Author:
Affiliation:
1. The RAND Corporation and California Institute of Technology,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.1896
Reference39 articles.
1. Second Approximation to Supersonic Conical Flows
2. SUPERSONIC FLOW PAST SLENDER POINTED BODIES OF REVOLUTION AT YAW
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